| 摘要 |
<p>The aircraft (10) has a wing (12) fixed at an elongated fuselage (11) in a median part according to length of the fuselage. Motors (16, 17) are fixed at a rear end and a front end of the fuselage, and comprise turbines (163, 173) driving in rotation around contrarotating coaxial propellers (161, 162, 171, 172). One of the motors is a propfan-type motor. The propellers are arranged to produce respective pushing forces directed according to longitudinal direction (X) of the aircraft and directed forwardly along movement direction of the aircraft during flight.</p> |
